| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Adaptive simulations of flame acceleration and detonation transition in subsonic and supersonic mixtures
|
Zhao, Wandong
|
|
|
136 |
C |
p.
|
artikel
|
| 2 |
Aerodynamic and structural multidisciplinary optimization design method of fan rotors based on blade curvature constraints
|
Song, Zhaoyun
|
|
|
136 |
C |
p.
|
artikel
|
| 3 |
Aeroelastic analyses of functionally graded aluminium composite plates reinforced with graphene nanoplatelets under fluid-structural interaction
|
Liu, Jun
|
|
|
136 |
C |
p.
|
artikel
|
| 4 |
An adaptive state estimation for tracking hypersonic glide targets with model uncertainties
|
Huang, Jingshuai
|
|
|
136 |
C |
p.
|
artikel
|
| 5 |
Anti-disturbance attitude quantized control of flexible spacecraft via a triggering and quantization joint dynamic event-triggered mechanism
|
Zhu, Chunjie
|
|
|
136 |
C |
p.
|
artikel
|
| 6 |
A self-adaptive local diversity-preserving NSGA-II for the multidisciplinary design optimization of a miniaturized supersonic rocket
|
Yan, Hao
|
|
|
136 |
C |
p.
|
artikel
|
| 7 |
A weak fault identification method of micro-turbine blade based on sound pressure signal with LSTM networks
|
Zhang, Jingqi
|
|
|
136 |
C |
p.
|
artikel
|
| 8 |
Capturing dynamics of a space manipulator end-effector with snare capture and retract operations
|
Li, Haiquan
|
|
|
136 |
C |
p.
|
artikel
|
| 9 |
Compression after multiple impact strength of composite laminates prediction method based on machine learning approach
|
Zhao, Jingyu
|
|
|
136 |
C |
p.
|
artikel
|
| 10 |
Deep reinforcement learning method for turbofan engine acceleration optimization problem within full flight envelope
|
Fang, Juan
|
|
|
136 |
C |
p.
|
artikel
|
| 11 |
Deep residual neural network for predicting aerodynamic coefficient changes with ablation
|
Lee, Dong Ho
|
|
|
136 |
C |
p.
|
artikel
|
| 12 |
Design optimization of a transonic compressor blade with sweep and lean integrated with axial slot casing treatment
|
Lu, Bingxiao
|
|
|
136 |
C |
p.
|
artikel
|
| 13 |
Distributed bearing-based formation maneuver control of fixed-wing UAVs by finite-time orientation estimation
|
Zhang, Yuwei
|
|
|
136 |
C |
p.
|
artikel
|
| 14 |
Distributed cooperative obstacle avoidance and formation reconfiguration for multiple quadrotors: Theory and experiment
|
Guo, Jinjin
|
|
|
136 |
C |
p.
|
artikel
|
| 15 |
Editorial Board
|
|
|
|
136 |
C |
p.
|
artikel
|
| 16 |
Edney III type shock-shock interaction over a hemisphere cylinder
|
Kianvashrad, Nadia
|
|
|
136 |
C |
p.
|
artikel
|
| 17 |
Effects of sawtooth grooves on supersonic combustion
|
Zhang, Lan
|
|
|
136 |
C |
p.
|
artikel
|
| 18 |
Effects of the airfoil probes on the aerodynamic performance of a transonic compressor cascade
|
Zhang, Qingdian
|
|
|
136 |
C |
p.
|
artikel
|
| 19 |
Entropy generation and CO2 emission in presence of pulsating oscillations in a bifurcating thermoacoustic combustor with a Helmholtz resonator at off-design conditions
|
Guan, Yiheng
|
|
|
136 |
C |
p.
|
artikel
|
| 20 |
Error-free strapdown inertial navigation system numerical updating algorithm in the launch-centered Earth-fixed frame for hypersonic vehicles
|
Liu, Shangbo
|
|
|
136 |
C |
p.
|
artikel
|
| 21 |
Experimental and numerical investigations for turbine aerodynamic performance with different pressure side squealers and incidence angles
|
Chen, Yingjie
|
|
|
136 |
C |
p.
|
artikel
|
| 22 |
Flow field modeling of airfoil based on convolutional neural networks from transform domain perspective
|
Hu, Jiawei
|
|
|
136 |
C |
p.
|
artikel
|
| 23 |
Flow separation control and performance evaluation of an asymmetric diffuser using vortex generators
|
Lu, Frank K.
|
|
|
136 |
C |
p.
|
artikel
|
| 24 |
Impact angle constraint guidance law using fully-actuated system approach
|
Chen, Shiwei
|
|
|
136 |
C |
p.
|
artikel
|
| 25 |
Influence of upstream wall slope on aerodynamic properties of a rectangular cavity in rarefied hypersonic flows
|
Guo, Guangming
|
|
|
136 |
C |
p.
|
artikel
|
| 26 |
Influences of geometric parameters on serpentine nozzles for turbofan
|
Sun, Peng
|
|
|
136 |
C |
p.
|
artikel
|
| 27 |
Initial exploration of a compliance-based morphing fairing concept for hinged aerodynamic surfaces
|
Mahid, Nuhaadh Mohamed
|
|
|
136 |
C |
p.
|
artikel
|
| 28 |
Integral terminal sliding-mode-based singularity-free finite-time tracking control for entry vehicle with input saturation
|
Shen, Ganghui
|
|
|
136 |
C |
p.
|
artikel
|
| 29 |
Investigation of dynamic mixedness characteristics of a transverse acoustically excited turbulent jet by high-repetition-rate acetone tracer planar laser-induced fluorescence technique
|
Yan, Bo
|
|
|
136 |
C |
p.
|
artikel
|
| 30 |
Multi-objective aerodynamic optimization of an axisymmetric variable-geometry inlet with a Mach 5 design point
|
Wang, Changsheng
|
|
|
136 |
C |
p.
|
artikel
|
| 31 |
Neural network-based multi-point, multi-objective optimisation for transonic applications
|
Tejero, Fernando
|
|
|
136 |
C |
p.
|
artikel
|
| 32 |
Numerical investigation of scalloping effect on lobed nozzle flow features and thermal mixing performance
|
Hou, Rui
|
|
|
136 |
C |
p.
|
artikel
|
| 33 |
Numerical investigation of the unstart flow at off-design condition of REST inlet at a Mach of 4
|
Zhong, Jiaxiang
|
|
|
136 |
C |
p.
|
artikel
|
| 34 |
Numerical investigations of the nozzle performance for a rocket-based rotating detonation engine with film cooling
|
Li, Rui
|
|
|
136 |
C |
p.
|
artikel
|
| 35 |
Numerical study on the deflagration to detonation transition promoted by transverse jet
|
Zhang, Zixu
|
|
|
136 |
C |
p.
|
artikel
|
| 36 |
Observer-based optimal control method combination with event-triggered strategy for hypersonic morphing vehicle
|
Bao, Cunyu
|
|
|
136 |
C |
p.
|
artikel
|
| 37 |
Online time-varying navigation ratio identification and state estimation of cooperative attack
|
Wang, Yinhan
|
|
|
136 |
C |
p.
|
artikel
|
| 38 |
Parametric aeroelastic modeling, maneuver loads analysis using CFD methods and structural design of a fighter aircraft
|
Voß, A.
|
|
|
136 |
C |
p.
|
artikel
|
| 39 |
Prescribed performance-based robust inverse optimal control for spacecraft proximity operations with safety concern
|
Li, Qi
|
|
|
136 |
C |
p.
|
artikel
|
| 40 |
Quantifying and mitigating uncertainties in design optimization including off-the-shelf components: Application to an electric multirotor UAV
|
Pollet, F.
|
|
|
136 |
C |
p.
|
artikel
|
| 41 |
Reinforcement learning with prior policy guidance for motion planning of dual-arm free-floating space robot
|
Cao, Yuxue
|
|
|
136 |
C |
p.
|
artikel
|
| 42 |
Simulation on atomization process of gas–liquid pintle injector in LRE under periodic conditions based on the VOF to DPM method
|
Shi, Pu
|
|
|
136 |
C |
p.
|
artikel
|
| 43 |
Sparse online Gaussian process adaptation for incremental backstepping flight control
|
Ignatyev, Dmitry I.
|
|
|
136 |
C |
p.
|
artikel
|
| 44 |
Study of multiple solution phenomenon for hypersonic air inlet
|
Tang, Xiao
|
|
|
136 |
C |
p.
|
artikel
|
| 45 |
The influence of the adverse pressure gradient on the flow characteristics of a serpentine nozzle with film cooling
|
Hui, Zhonghao
|
|
|
136 |
C |
p.
|
artikel
|
| 46 |
The role of HMX particle size in the combustion and agglomeration of HTPB-based propellant
|
Gou, Dongliang
|
|
|
136 |
C |
p.
|
artikel
|
| 47 |
Trajectory planning for satellite cluster reconfigurations with sequential convex programming method
|
Wang, Lixiang
|
|
|
136 |
C |
p.
|
artikel
|
| 48 |
Vortex structure for reducing tip leakage flow of linear turbine cascade using dielectric barrier discharge plasma actuator
|
Matsunuma, Takayuki
|
|
|
136 |
C |
p.
|
artikel
|
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